Add to ORKGA cooperative flight test by NASA, Bell Helicopter and the U.S. Army to characterize the steady state acoustics and measure the maneuver noise of a Bell Helicopter 430 aircraft was accomplished. The test occurred during June/July, 2011 at Eglin Air Force Base, Florida. This test gathered a total of 410 data points over 10 test days and compiled an extensive data base of dynamic maneuver measurements. Three microphone configurations with up to 31 microphones in each configuration were used to acquire acoustic data. Aircraft data included DGPS, aircraft state and rotor state information. This paper provides an overview of the test
PDFTech ReportFAA-EE-85-6HelicoptersFlight testsAircraft noiseMeasurementStandardsStandardizationCer...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
A new model for estimating the noise radiation during maneuvering flight is developed in this paper....
A cooperative ight test by NASA, Bell Helicopter and the U.S. Army to characterize the steady state ...
acoustics and measure the maneuver noise of a Bell Helicopter 430 aircraft was accomplished. The tes...
A special acoustic flight test program was performed on the Bell 206B helicopter outfitted with an i...
Two acoustic flight tests have been conducted on a remote test range at Eglin Air Force Base in the ...
FA353/A3008The U.S. Department of Transportation, Federal Aviation Administration, (U.S.DOT/FAA),alo...
This paper presents the test design, instrumentation set-up, data acquisition, and the results of an...
To evaluate the noise reduction potential for tiltrotor aircraft, a series of three XV- 15 acoustic ...
This document presents acoustical data and flight path information acquired during the FAA/HAI Helic...
This report documents the results of a Federal Aviation Administration (FAA) noise measurement fligh...
The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics...
This paper presents an overview of a flight test campaign performed at different test sites whose al...
XV-15 acoustic test is discussed, and measured results are presented. The test was conducted by NASA...
PDFTech ReportFAA-EE-85-6HelicoptersFlight testsAircraft noiseMeasurementStandardsStandardizationCer...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
A new model for estimating the noise radiation during maneuvering flight is developed in this paper....
A cooperative ight test by NASA, Bell Helicopter and the U.S. Army to characterize the steady state ...
acoustics and measure the maneuver noise of a Bell Helicopter 430 aircraft was accomplished. The tes...
A special acoustic flight test program was performed on the Bell 206B helicopter outfitted with an i...
Two acoustic flight tests have been conducted on a remote test range at Eglin Air Force Base in the ...
FA353/A3008The U.S. Department of Transportation, Federal Aviation Administration, (U.S.DOT/FAA),alo...
This paper presents the test design, instrumentation set-up, data acquisition, and the results of an...
To evaluate the noise reduction potential for tiltrotor aircraft, a series of three XV- 15 acoustic ...
This document presents acoustical data and flight path information acquired during the FAA/HAI Helic...
This report documents the results of a Federal Aviation Administration (FAA) noise measurement fligh...
The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics...
This paper presents an overview of a flight test campaign performed at different test sites whose al...
XV-15 acoustic test is discussed, and measured results are presented. The test was conducted by NASA...
PDFTech ReportFAA-EE-85-6HelicoptersFlight testsAircraft noiseMeasurementStandardsStandardizationCer...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
A new model for estimating the noise radiation during maneuvering flight is developed in this paper....